We present here a numerical study of the aeroelastic behavior of a pressurized flexible airship (blimp) during a flight with an angle of attack of 20. The airship is represented by a 6:1 prolate spheroid generic geometry . The air flow is fully turbulent and is modeled by a LES model. We solve the Navier-Stokes three-dimensional compressible equations in their ALE form. The spatial discretization of these equations is achieved on unstructured tetrahedral meshes by a Finite Volumes/Finite Elements (FV/FE) mixed formulation.
This fluid simulation is coupled to a structure solver by a staggered algorithm.
We investigate a flexible pressurized hull compared to a non-pressurized one
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